博碩士論文 100323002 完整後設資料紀錄

DC 欄位 語言
DC.contributor機械工程學系zh_TW
DC.creator徐宏鈞zh_TW
DC.creatorShiu Hungjiunen_US
dc.date.accessioned2013-6-18T07:39:07Z
dc.date.available2013-6-18T07:39:07Z
dc.date.issued2013
dc.identifier.urihttp://ir.lib.ncu.edu.tw:88/thesis/view_etd.asp?URN=100323002
dc.contributor.department機械工程學系zh_TW
DC.description國立中央大學zh_TW
DC.descriptionNational Central Universityen_US
dc.description.abstract本研究是運用超塑成形技術(Superplastic Forming Technology)實驗製作(原始工件尺寸及縮小版)中型民航機機翼前緣(Leading Edge)之整流罩(Fairing Cover)、研究探討其成形方式(如熱引伸輔助超塑成形及直接超塑成形)與模具輪廓對於成形後厚度分布的影響。 在執行超塑成形之前,先將超塑鋁合金5083材料進行預折彎加工,在依其所需之氣壓-時間成形曲線來完成工件,預折彎之目的在於使鈑材在執行超塑成形之前,可預先縮短鈑片與成形模具之間的距離,使其工件成形後之厚度分布均勻性更佳。 探討成形距離之重要性後,決定於模具設計熱引伸輔助的加工程序或是改變模具的輪廓設計,來進一步縮短該成形距離,以期此工件可以有更佳的厚度分布均勻性。zh_TW
dc.description.abstractThis paper is using superplastic forming technology to produce (original size and small size) medium-sized civil aircraft wing leading edge fairing cover. To analyze the influence of forming method (hot draw mechanical pre-forming and conventional superplastic forming) and die contour on thickness distribution. Before doing the superplastic forming, first, we pre-bend the 5083 aluminum , then make the component according to the required pressure - time forming curves. The purpose of the pre-bend is to shorten the distance between the sheet and the die before doing the superplastic forming, As a results, the thickness of the component will more uniform. After realizing the importance of shorten the forming distance, we decide to add a hot drawing mechanical pre-forming or change the contour of the die to shorten the distance. We hope that the thickness of the component will more uniform.en_US
DC.subject超塑成形zh_TW
DC.subject5083鋁合金zh_TW
DC.subjectSuperplastic formingen_US
DC.subjectAluminum 5083en_US
DC.title超塑成形模具輪廓設計對其成形厚度之影響zh_TW
dc.language.isozh-TWzh-TW
DC.titleThe Influence of Superplastic Forming Die Contour on Thickness Distributionen_US
DC.type博碩士論文zh_TW
DC.typethesisen_US
DC.publisherNational Central Universityen_US

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